DE60327941D1 - CHAFTSKOMBINATIONEN - Google Patents

CHAFTSKOMBINATIONEN

Info

Publication number
DE60327941D1
DE60327941D1 DE60327941T DE60327941T DE60327941D1 DE 60327941 D1 DE60327941 D1 DE 60327941D1 DE 60327941 T DE60327941 T DE 60327941T DE 60327941 T DE60327941 T DE 60327941T DE 60327941 D1 DE60327941 D1 DE 60327941D1
Authority
DE
Germany
Prior art keywords
alloy product
fatigue failure
improved fatigue
failure resistance
chaftskombinationen
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60327941T
Other languages
German (de)
Inventor
Gary H Bray
John Liu
Lynn Eugene Oswald
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Howmet Aerospace Inc
Original Assignee
Alcoa Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=32326381&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE60327941(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Alcoa Inc filed Critical Alcoa Inc
Application granted granted Critical
Publication of DE60327941D1 publication Critical patent/DE60327941D1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/10—Alloys based on aluminium with zinc as the next major constituent

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Laminated Bodies (AREA)
  • Conductive Materials (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Secondary Cells (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

An alloy product having improved fatigue failure resistance, comprising about, by weight, 7.6 to about 8.4% zinc, about 2.0 to about 2.6% copper, about 1.8 to about 2.3% magnesium, about 0.088 to about 0.25% Zr, about 0.01 to about 0.09% Fe, and about 0.01 to about 0.06% Si, the balance substantially aluminium and incidental elements and impurities. The alloy product, suitable for aerospace applications, exhibits improved fatigue failure resistance than its 7055 counterpart of similar size, shape, thickness and temper.
DE60327941T 2002-11-15 2003-11-17 CHAFTSKOMBINATIONEN Expired - Lifetime DE60327941D1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US42659702P 2002-11-15 2002-11-15
PCT/US2003/036490 WO2004046403A2 (en) 2002-11-15 2003-11-17 Aluminum alloy product having improved combinations of properties

Publications (1)

Publication Number Publication Date
DE60327941D1 true DE60327941D1 (en) 2009-07-23

Family

ID=32326381

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60327941T Expired - Lifetime DE60327941D1 (en) 2002-11-15 2003-11-17 CHAFTSKOMBINATIONEN

Country Status (9)

Country Link
US (1) US7097719B2 (en)
EP (3) EP2080816A1 (en)
AT (1) ATE433503T1 (en)
AU (1) AU2003290922A1 (en)
BR (1) BRPI0315625B8 (en)
CA (1) CA2506393C (en)
DE (1) DE60327941D1 (en)
ES (1) ES2329674T3 (en)
WO (1) WO2004046403A2 (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050034794A1 (en) * 2003-04-10 2005-02-17 Rinze Benedictus High strength Al-Zn alloy and method for producing such an alloy product
CN100547098C (en) * 2003-04-10 2009-10-07 克里斯铝轧制品有限公司 A kind of Al-zn-mg-cu alloy
US7883591B2 (en) * 2004-10-05 2011-02-08 Aleris Aluminum Koblenz Gmbh High-strength, high toughness Al-Zn alloy product and method for producing such product
EP1683882B2 (en) 2005-01-19 2010-07-21 Otto Fuchs KG Aluminium alloy with low quench sensitivity and process for the manufacture of a semi-finished product of this alloy
US20060213591A1 (en) 2005-03-24 2006-09-28 Brooks Charles E High strength aluminum alloys and process for making the same
US20070204937A1 (en) * 2005-07-21 2007-09-06 Aleris Koblenz Aluminum Gmbh Wrought aluminium aa7000-series alloy product and method of producing said product
US8083871B2 (en) 2005-10-28 2011-12-27 Automotive Casting Technology, Inc. High crashworthiness Al-Si-Mg alloy and methods for producing automotive casting
WO2008003503A2 (en) * 2006-07-07 2008-01-10 Aleris Aluminum Koblenz Gmbh Method of manufacturing aa2000 - series aluminium alloy products
FR2907796B1 (en) * 2006-07-07 2011-06-10 Aleris Aluminum Koblenz Gmbh ALUMINUM ALLOY PRODUCTS OF THE AA7000 SERIES AND METHOD FOR MANUFACTURING THE SAME
US8673209B2 (en) 2007-05-14 2014-03-18 Alcoa Inc. Aluminum alloy products having improved property combinations and method for artificially aging same
US8840737B2 (en) * 2007-05-14 2014-09-23 Alcoa Inc. Aluminum alloy products having improved property combinations and method for artificially aging same
US8333853B2 (en) * 2009-01-16 2012-12-18 Alcoa Inc. Aging of aluminum alloys for improved combination of fatigue performance and strength
US8206517B1 (en) 2009-01-20 2012-06-26 Alcoa Inc. Aluminum alloys having improved ballistics and armor protection performance
US9163304B2 (en) 2010-04-20 2015-10-20 Alcoa Inc. High strength forged aluminum alloy products
CN104321451A (en) * 2012-03-07 2015-01-28 美铝公司 Improved 7XXX aluminum alloys, and methods for producing the same
US9587298B2 (en) 2013-02-19 2017-03-07 Arconic Inc. Heat treatable aluminum alloys having magnesium and zinc and methods for producing the same
RU2556849C1 (en) * 2014-04-14 2015-07-20 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") High-strength heat-treatable aluminium alloy and article made thereof
CA3100242C (en) 2018-06-12 2023-08-08 Aleris Rolled Products Germany Gmbh Method of manufacturing a 7xxx-series aluminium alloy plate product having improved fatigue failure resistance
CN108754258A (en) * 2018-06-26 2018-11-06 安徽沪源铝业有限公司 7055 aluminium alloys of one kind and its aging technique

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4305763A (en) * 1978-09-29 1981-12-15 The Boeing Company Method of producing an aluminum alloy product
US5108520A (en) 1980-02-27 1992-04-28 Aluminum Company Of America Heat treatment of precipitation hardening alloys
US5221377A (en) * 1987-09-21 1993-06-22 Aluminum Company Of America Aluminum alloy product having improved combinations of properties
US5277719A (en) * 1991-04-18 1994-01-11 Aluminum Company Of America Aluminum alloy thick plate product and method
US6027582A (en) * 1996-01-25 2000-02-22 Pechiney Rhenalu Thick alZnMgCu alloy products with improved properties
US7135077B2 (en) * 2000-05-24 2006-11-14 Pechiney Rhenalu Thick products made of heat-treatable aluminum alloy with improved toughness and process for manufacturing these products
CN1489637A (en) * 2000-12-21 2004-04-14 �Ƹ��� Aluminum alloy products and artificial aging method

Also Published As

Publication number Publication date
WO2004046403A2 (en) 2004-06-03
EP2309011A3 (en) 2013-05-08
ES2329674T3 (en) 2009-11-30
EP1565586A4 (en) 2006-08-02
US7097719B2 (en) 2006-08-29
ATE433503T1 (en) 2009-06-15
EP2080816A1 (en) 2009-07-22
EP2309011A2 (en) 2011-04-13
BR0315625A (en) 2005-08-23
CA2506393A1 (en) 2004-06-03
CA2506393C (en) 2009-10-27
WO2004046403A3 (en) 2004-07-01
US20040136862A1 (en) 2004-07-15
AU2003290922A8 (en) 2004-06-15
AU2003290922A1 (en) 2004-06-15
BRPI0315625B1 (en) 2013-06-04
EP1565586B1 (en) 2009-06-10
EP1565586A2 (en) 2005-08-24
BRPI0315625B8 (en) 2022-11-08

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8328 Change in the person/name/address of the agent

Representative=s name: LENZING GERBER STUTE PARTNERSCHAFTSGESELLSCHAFT VO